WO2010070185A3 - Aircraft stabiliser trailing edge - Google Patents

Aircraft stabiliser trailing edge Download PDF

Info

Publication number
WO2010070185A3
WO2010070185A3 PCT/ES2009/070609 ES2009070609W WO2010070185A3 WO 2010070185 A3 WO2010070185 A3 WO 2010070185A3 ES 2009070609 W ES2009070609 W ES 2009070609W WO 2010070185 A3 WO2010070185 A3 WO 2010070185A3
Authority
WO
WIPO (PCT)
Prior art keywords
stabiliser
trailing edge
aircraft
clip
coupling element
Prior art date
Application number
PCT/ES2009/070609
Other languages
Spanish (es)
French (fr)
Other versions
WO2010070185A2 (en
Inventor
Alberto BALSA GONZÁLEZ
Francisco De Paula Burgos Gallego
Original Assignee
Airbus Operations, S.L.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations, S.L. filed Critical Airbus Operations, S.L.
Priority to CN200980155875.6A priority Critical patent/CN102300770B/en
Publication of WO2010070185A2 publication Critical patent/WO2010070185A2/en
Publication of WO2010070185A3 publication Critical patent/WO2010070185A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/02—Tailplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders

Abstract

The invention relates to the trailing edge (3) of an aircraft stabiliser (1) which is made from a composite material and includes an outer skin (40) and an inner skin (41) which are joined to the trailing edge (3) by means of clip-type coupling element (20). The invention is characterised in that the ends of the clip-type coupling element (20) include recesses (23) intended to be coupled to the inner area of the upper and lower skins (40, 41) of the stabiliser (1), said clip-type coupling element being sufficiently flexible for it to be clipped in such a way that the ends are housed by means of the aforementioned recesses (23) between the outer and inner skins (40, 41) of the aircraft stabiliser (1), so that the outer area on the trailing edge (3) of the stabiliser (1) is formed by a continuous aerodynamic surface without any changes in slope.
PCT/ES2009/070609 2008-12-18 2009-12-18 Aircraft stabiliser trailing edge WO2010070185A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200980155875.6A CN102300770B (en) 2008-12-18 2009-12-18 Aircraft stabiliser surface trailing edge

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ESP200803603 2008-12-18
ES200803603A ES2367935B1 (en) 2008-12-18 2008-12-18 AIRCRAFT STABILIZING SURFACE OUTPUT EDGE.

Publications (2)

Publication Number Publication Date
WO2010070185A2 WO2010070185A2 (en) 2010-06-24
WO2010070185A3 true WO2010070185A3 (en) 2010-08-12

Family

ID=42173173

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2009/070609 WO2010070185A2 (en) 2008-12-18 2009-12-18 Aircraft stabiliser trailing edge

Country Status (4)

Country Link
US (1) US8444091B2 (en)
CN (1) CN102300770B (en)
ES (1) ES2367935B1 (en)
WO (1) WO2010070185A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106567990A (en) * 2015-10-10 2017-04-19 陕西飞机工业（集团）有限公司 Foam filling structure and processing method thereof

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2371401B1 (en) * 2008-06-27 2012-11-07 Airbus Operations, S.L. AIRCRAFT SUSTAINER SURFACE STRUCTURE.
GB201004757D0 (en) * 2010-03-23 2010-05-05 Airbus Operations Ltd Joint
FR2973774B1 (en) 2011-04-06 2015-05-08 Airbus Operations Sas METHOD FOR IMPROVING THE AERODYNAMIC EFFICIENCY OF A VERTICAL AIRCRAFT TENSION
ES2421410B1 (en) * 2012-02-29 2014-10-28 Airbus Operations, S.L. EDGE EDGE OF AN AIRCRAFT SURFACE OF AN AIRCRAFT
US10173789B2 (en) * 2012-04-02 2019-01-08 Aerosud Technology Solutions (Pty) Ltd. Cellular core composite leading and trailing edges
US9352822B2 (en) * 2012-05-30 2016-05-31 The Boeing Company Bonded composite airfoil
EP2698241B1 (en) * 2012-08-16 2016-04-27 Airbus Operations S.L. Highly integrated inner structure of a torsion box of an aircraft lifting surface and method of producing it
US10329009B2 (en) * 2014-09-17 2019-06-25 The Boeing Company Composite wing edge attachment and method
EP3210883B1 (en) * 2016-02-29 2020-01-29 Airbus Operations, S.L. Aircraft airfoil having a stitched trailing edge and manufacturing method thereof
CN107434031A (en) 2016-05-25 2017-12-05 空中客车简化股份公司 The structure member of aircraft wing body and the aircraft including the structure member
US10532804B2 (en) 2017-02-08 2020-01-14 The Boeing Company Aerodynamic control surface and associated trailing edge close-out method
CN109606637A (en) * 2018-11-02 2019-04-12 中国航空工业集团公司西安飞机设计研究所 A kind of Composite Sandwich wall panel structure of general-purpose aircraft rudder
EP3683139B1 (en) * 2019-01-18 2021-07-28 Airbus Operations, S.L.U. Flight control surface for an aircraft and method for manufacturing said flight control surface
CN112093029A (en) * 2019-06-18 2020-12-18 成都飞机工业（集团）有限责任公司 Aircraft airfoil trailing edge
CN114771802A (en) * 2021-01-22 2022-07-22 波音公司 Aerodynamic structure and method of forming an aerodynamic structure
EP4155192A1 (en) * 2021-09-28 2023-03-29 Airbus Operations, S.L.U. Profile for a trailing edge of an airfoil and method to repair thereof

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214092B (en) * 1963-06-08 1966-04-07 Monte Copter Inc Aircraft wing, in particular rotary wing, which can be assembled from two or more parts in the depth direction
US20040000613A1 (en) * 2002-06-28 2004-01-01 Thomas William A. Preforms for acute structural edges

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2193951A (en) * 1937-05-28 1940-03-19 John H Van Uum Spring clip device
US2613893A (en) * 1948-04-01 1952-10-14 Curtiss Wright Corp Airfoil construction
CN100455793C (en) * 2003-03-31 2009-01-28 丹麦技术大学 Control of power, loads and/or stability of a horizontal axis wind turbine by use of variable blade geometry control

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214092B (en) * 1963-06-08 1966-04-07 Monte Copter Inc Aircraft wing, in particular rotary wing, which can be assembled from two or more parts in the depth direction
US20040000613A1 (en) * 2002-06-28 2004-01-01 Thomas William A. Preforms for acute structural edges

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106567990A (en) * 2015-10-10 2017-04-19 陕西飞机工业（集团）有限公司 Foam filling structure and processing method thereof

Also Published As

Publication number Publication date
ES2367935B1 (en) 2012-09-18
US8444091B2 (en) 2013-05-21
CN102300770B (en) 2015-03-04
CN102300770A (en) 2011-12-28
WO2010070185A2 (en) 2010-06-24
US20100155528A1 (en) 2010-06-24
ES2367935A1 (en) 2011-11-11

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